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Manufacturer | Piper Aircraft |
---|---|
Model | PA-28-161 Warrior II |
Engine | Lycoming O-320-D3G |
Horsepower | 160 hp |
Seating Capacity | 4 |
Wingspan | 35 ft (10.7 m) |
Length | 24 ft 0 in |
Maximum Speed | 127 knots |
Cruise Speed | 122 knots |
Maximum Takeoff Weight | 2, 325 lb (1, 055 kg) |
Fuel Capacity | 48 US gallons (182 L) |
Outlines critical operating limitations for safe flight.
Detailed procedures for handling various in-flight emergencies.
Step-by-step instructions for standard aircraft operations.
Covers performance data, charts, and flight planning information.
Procedures for determining and maintaining aircraft weight and balance.
Defines critical airspeeds like Never Exceed, Cruising, Best Climb Angle/Rate.
Lists maximum weights and baggage space.
Introduces the limitations section covering placards and markings.
Lists critical airspeed limitations (VNE, VNO, VFE) and power plant limits.
Specifies acceptable weight, C.G. range, and maneuver limits.
A concise checklist covering critical emergency situations for quick reference.
Procedures for engine fire during start, power loss during takeoff and flight.
Detailed steps for power-off landings and handling fires during flight.
Procedures for electrical failures, overloads, and spin recovery.
Procedures for addressing carburetor icing and engine roughness.
Overview of normal procedures and significant airspeeds for safe operation.
Describes the fuel system, selector, pump, and electrical system components.
General guidelines, warnings about non-Piper parts, and modification approvals.
Safety tips for engine start, anti-collision lights, and rudder pedal use.